This paper discusses a precision attitude and control technique for meeting these requirements utilizing a similar architecture that was adopted for the Laboratory of Atmospheric and Space Physics (LASP) SNOE (Student Nitrous Oxide Explorer) spinning spacecraft; SNOE has been operating with its ADCS architecture in low earth orbit (LEO) for over two years.


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    Titel :

    Precision ADCS of a spinning spacecraft for the Mars Aeronomy Explorer Mission


    Beteiligte:
    Mungas, Greg S. (Autor:in) / Shotwell, Robert (Autor:in) / Gray, Andrew (Autor:in)

    Kongress:

    96th AIAA Aerospace Control and Guidance Systems Committee Meeting ; 2005 ; Hilton Head, SC, United States


    Erscheinungsdatum :

    19.10.2005


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




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